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181   $ctxt$2rdacontent
182   $cc$2rdamedia
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200 10$aFlight demonstration of a shock location sensor using constant voltage hot-film anemometry /$fTimothy R. Moes, Garimella R. Sarma and Siva M. Mangalam
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,$dAugust 1997.
215   $a1 online resource (25 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4806
300   $aTitle from title screen (viewed March 30, 2016).
300   $a"August 1997."
300   $a"Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.
320   $aIncludes bibliographical references (page 25).
606   $aTransonic speed$2nasat
606   $aLeading edges$2nasat
606   $aLaminar boundary layer$2nasat
606   $aHot-film anemometers$2nasat
606   $aAirfoils$2nasat
615  7$aTransonic speed.
615  7$aLeading edges.
615  7$aLaminar boundary layer.
615  7$aHot-film anemometers.
615  7$aAirfoils.
700   $aMoes$b Timothy R.$01386042
702   $aSarma$b Garimella R.
702   $aMangalam$b Siva M.
712 02$aNASA Dryden Flight Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
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996   $aFlight demonstration of a shock location sensor using constant voltage hot-film anemometry$93522591
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